| setReferenceState(SpacecraftState) |  | 100% |  | 91% | 1 | 7 | 0 | 35 | 0 | 1 |
| getParametersJacobian(SpacecraftState) | | 100% | | 90% | 1 | 6 | 0 | 11 | 0 | 1 |
| addToRow(double[], int) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getStateTransitionMatrix(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| setInitialStm(String, RealMatrix) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getJacobiansColumnsNames() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| updateDerivativesIfNeeded(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getAdditionalData(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| freezeColumnsNames() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |